# N298SK: 2001 Embraer EMB-145LR, registration cancelled 2023-06-01 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 1, 2023 - Status when cancelled: Valid registration - Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212) - Engine: [Rolls-Royce AE-3007A1P](https://openairdocs.org/engine/rolls-royce-ae-3007a1p) (registry code 54571) - Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Serial number: 145508 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 27, 2001 - Certificate issued: May 14, 2018 - Last registry action: May 12, 2023 - Mode S code: A314CC - Owner when cancelled: [Southern Aircraft Consultancy Inc Trustee](https://openairdocs.org/faa-owner/SOUTHERN%20AIRCRAFT%20CONSULTANCY%20INC%20TRUSTEE) - Location: Bergh Apton Nflk, United Kingdom - Owner type: Corporation - The mark today: https://openairdocs.org/aircraft/N298SK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=298SK - Page: https://openairdocs.org/deregistered/N298SK-2023-06-01 From the FAA registry file of November 7, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Embraer EMB-145LR: https://openairdocs.org/model/embraer-emb-145lr.md ## Service difficulty reports (32) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UHLA201504300345](https://openairdocs.org/sdr/UHLA201504300345), Apr 30, 2015: SHEAR TIE. CRACKED. DURING INSPECITON, A CRACK WAS FOUND ON THE SHEAR TIE AT FRAME 67 AND STRINGERS 6-7L. THE SHEAR TIE WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA201504300344](https://openairdocs.org/sdr/UHLA201504300344), Apr 30, 2015: SHEAR TIE. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR TIE AT FRAME 68 AND STRINGERS 8L AND 9L THE SHEAR TIE WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015033100221](https://openairdocs.org/sdr/UHLA2015033100221), Mar 31, 2015: CONTROLLER. INOPERATIVE. THE CREW REPORTED THAT THE CABIN ALTITUDE INDICATION DASHED IN FLIGHT. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED UNEVENTFULLY AT ITS INTENDED DESTINAT - [SDR CHQA20140916259](https://openairdocs.org/sdr/CHQA20140916259), Sep 16, 2014: AHRS. FAULTY. THE ACFT WAS TO BE FERRIED FOR MAINTENANCE DUE TO AN AHRS 1 INOPERATIVE MSG. BEFORE THE FLIGHT THE AHRS 1 WAS SWAPPED WITH THE AHRS 2. DURING THE FERRY FLIGHT T - [SDR CHQA20140309077](https://openairdocs.org/sdr/CHQA20140309077), Mar 9, 2014: FLAP. MALFUNCTIONED. CREW REPORTED THAT THEY RECEIVED A FLAP FAIL MSG DURING FLIGHT. THE CREW DECLARED AN EMERGENCY & LANDED AT THEIR INTENDED DESTINATION WITHOUT INCIDENT. MX RESET - [SDR CHQA20140203059](https://openairdocs.org/sdr/CHQA20140203059), Feb 3, 2014: DOUBLER. DAMAGED. DURING INSPECTION, A PREVIOUS REPAIR AT THE EXTERNAL POWER DOOR AT FRAME 7 WAS FOUND TO BE DAMAGED. THE REPAIR DOUBLER WAS REPLACED IAW ETD 2014-145-010498 REVI - [SDR CHQA20140131057](https://openairdocs.org/sdr/CHQA20140131057), Jan 31, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RT OMEGA BEAM AT FRAME 24. THE BEAM WAS REPAIRED IAW ETD 2014-145-008961. - [SDR CHQA20140130058](https://openairdocs.org/sdr/CHQA20140130058), Jan 30, 2014: FITTING. CRACKED. DURING INSPECTION, THE SHEAR CLIP AT FRAME 24 & STRINGERS 15R TO 16R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140130056](https://openairdocs.org/sdr/CHQA20140130056), Jan 30, 2014: STIFFENER. CRACKED. DURING INSPECTION, THE STIFFENER AT FRAME 20, STRINGER 3L WAS FOUND TO BE CRACKED. THE STIFFENER WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20130315080](https://openairdocs.org/sdr/CHQA20130315080), Mar 15, 2013: PROBE. DEFECTIVE. CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A TAT 1 HEAT INOP MESSAGE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. THE MESSAGE CLEARED UPON LANDI - [SDR CHQA20120319102](https://openairdocs.org/sdr/CHQA20120319102), Mar 19, 2012: DOOR FRAME. CRACKED. DURING INSPECTION, FRAME 67 WAS FOUND TO BE CRACKED AT THE CARGO DOOR ENTRANCE. FRAME 67 AT THE CARGO DOOR ENTRANCE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145 - [SDR CHQA20120319101](https://openairdocs.org/sdr/CHQA20120319101), Mar 19, 2012: DOOR FRAME. CRACKED. DURING INSPECTION, FRAME 66 WAS FOUND TO BE CRACKED AT THE CARGO DOOR ENTRANCE. FRAME 66 AT THE CARGO DOOR ENTRANCE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145 - [SDR CHQA 20120318105](https://openairdocs.org/sdr/CHQA%2020120318105), Mar 18, 2012: SPAR CAP. CHAFED. DURING INSPECTION, THE VERTICAL FIN LEADING EDGE LEFT AND RIGHT FORWARD SPAR CAPS WAS FOUND THE BE CHAFED. THE VERTICAL FIN LEADING EDGE LEFT AND RIGHT FORWARD - [SDR CHQA20120318104](https://openairdocs.org/sdr/CHQA20120318104), Mar 18, 2012: SPAR CAP. CHAFED. DURING INSPECTION, THE VERTICAL FIN LEADING EDGE LEFT AND RIGHT FORWARD SPAR CAPS WAS FOUND THE BE CHAFED. THE VERTICAL FIN LEADING EDGE LEFT AND RIGHT FORWARD - [SDR CHQA20120317100](https://openairdocs.org/sdr/CHQA20120317100), Mar 17, 2012: STRINGER. DAMAGED. DURING INSPECTION, TOOL MARKS WERE FOUND ON STRINGER 19R SPLICE BETWEEN FRAME 52 AND FRAME 53. STRINGER 19R SPLICE BETWEEN FRAME 52 AND FRAME 53 WAS REPAIRED IN - [SDR CHQA20120316103](https://openairdocs.org/sdr/CHQA20120316103), Mar 16, 2012: SKIN. DAMAGED. DURING INSPECTION, THE LEFT SKIN DAMAGE WAS FOUND ON RUDDER II AT THE PROTRACTOR NUT PLATE ATTACHMENT. THE LEFT SKIN ON RUDDER II AT THE PROTRACTOR NUT PLACE WA - [SDR CHQA20120316099](https://openairdocs.org/sdr/CHQA20120316099), Mar 16, 2012: FRAME. CRACKED. DURING INSPECTION THE LEFT AND RIGHT FRAME 10 WERE FOUND TO BE CRACKED. MAINTENANCE REPLACED THE LEFT AND RIGHT FRAME 10. THE NEW PARTS WERE INSTALLED WITH A SO - [SDR CHQA20120316098](https://openairdocs.org/sdr/CHQA20120316098), Mar 16, 2012: FRAME. CRACKED. DURING INSPECTION THE LEFT AND RIGHT FRAME 10 WERE FOUND TO BE CRACKED. MAINTENANCE REPLACED THE LEFT AND RIGHT FRAME 10. THE NEW PARTS WERE INSTALLED WITH A SO - [SDR CHQA20120316097](https://openairdocs.org/sdr/CHQA20120316097), Mar 16, 2012: FLOOR SUPPORT. CRACKED. DURING INSPECTION, THE CENTER FUSELAGE III RIGHT OMEGA BEAM WAS FOUND TO BE CRACKED. THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORDANCE W - [SDR CHQA20120316096](https://openairdocs.org/sdr/CHQA20120316096), Mar 16, 2012: BEAM. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT LOWER BEAM. THE LOWER BEAM ON THE CARGO DOOR CUTOUT WAS REPLACED. THE NEW PART WAS INSTALLED WIT - [SDR CHQA20120316095](https://openairdocs.org/sdr/CHQA20120316095), Mar 16, 2012: STRUCTURE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR STRUCTURE FORWARD L-SHAPE. THE L-SHAPE ON THE FORWARD CARGO DOOR SURROUND WAS REPAIRED IN ACCORDANCE WI - [SDR CHQA20120214051](https://openairdocs.org/sdr/CHQA20120214051), Feb 14, 2012: BATTERY PACK. DISCHARGED. DURING INSPECTION, 2 FLOOR STRIP EMERGENCY PROXIMITY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER TWO EMERGENCY BATTERY PACK. OPERATIONA - [SDR CHQA201100373](https://openairdocs.org/sdr/CHQA201100373), Sep 14, 2011: LIGHT. MALFUNCTIONED. CREW REPORTED THAT THE LEFT-HAND UPPER WING EMERGENCY LIGHT WAS INOPERATIVE. THE EMERGENCY LIGHT WAS DEFERRED. MAINTENANCE CLEARED THE DEFERRAL ON 9/15/2011 BY - [SDR CHQA201000177](https://openairdocs.org/sdr/CHQA201000177), Sep 10, 2010: WIRE. BROKEN. DURING INSPECTION THE LEFT NR 1 FLOOR PROXIMITY EMERGENCY LIGHT WAS FOUND TO HAVE BROKEN WIRES. THIS AIRCRAFT IS CURRENTLY IN C-CHECK. MAINTENANCE REPAIRED THE - [SDR CHQA201000176](https://openairdocs.org/sdr/CHQA201000176), Sep 10, 2010: WIRE. BROKEN. DURING INSPECTION THE LEFT EMERGENCY LIGHT ON PANEL 191 WAS FOUND TO HAVE BROKEN WIRES. THIS AIRCRAFT IS CURRENTLY IN C-CHECK. MAINTENANCE REPAIRED THE WIRES TO - [SDR CHQA201000102](https://openairdocs.org/sdr/CHQA201000102), May 26, 2010: WARNING SYSTEM. MALFUNCTIONED. ON TAKEOFF FROM BWI, THE CREW RAISED THE LANDING GEAR HANDLE AND RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE ON EICAS, AND THE LEFT MAIN GEAR INDICATION WAS - [SDR CHQA201000087](https://openairdocs.org/sdr/CHQA201000087), Apr 27, 2010: LIGHT. INOPERATIVE. DURING INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND INOP. MAINTENANCE REPLACED THE LIGHT BULB IN THE RIGHT OVERWING EMERGENCY LIGHT WITH NO FURTHER - [SDR CHQA200900231](https://openairdocs.org/sdr/CHQA200900231), Oct 27, 2009: PROXIMITY SWITCH. DAMAGED. AFTER ROTATION THE CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE FOLLOWED BY A REVERSE DISAGREE MESSAGE. THE CREW FOLLOWED THE QRH AND RETURNED TO FIELD. - [SDR CHQA200900152](https://openairdocs.org/sdr/CHQA200900152), Jul 5, 2009: INVERTER. INOPERATIVE. DURING THE EMERGENCY LIGHT OPS CHECK, MX FOUND INVERTERS 2 AND 3 TO BE INOPERATIVE. THE NR 2 AND 3 INVERTERS WERE REPLACED AND THE EMERGENCY LIGHT SYS OPERATED - [SDR CHQA200700034](https://openairdocs.org/sdr/CHQA200700034), Jul 11, 2007: EXTINGUISHER. INOPERATIVE. FLIGHT 3052 - SAV-LGA - WHILE AT FL370, THE BAGGAGE FIRE EXTINGUISHER BUTTON LIT UP, NO EICAS OR AWU WARNING/MESSAGES DISPLAYED. UPON PRESSING THE BAGGAGE FIRE - [SDR CHQA200700018](https://openairdocs.org/sdr/CHQA200700018), May 20, 2007: SWITCH. MALFUNCTIONED. FLIGHT 3005 - PHL-GSO - AT FL270, RECEIVED FIRE BELL AND A RED "BAGG SMOKE" EICAS MESSAGE. RAN QRH, FIRED THE BAGGAGE FIRE EXTINGUISHING BOTTLES. MESSAGE REMAIN - [SDR CHQA200500149](https://openairdocs.org/sdr/CHQA200500149), Aug 28, 2005: LIGHT. INOPERATIVE. FIRST FLOOR EMERGENCY LIGHT STRIP INOPERATIVE. REMOVED AND REPLACED THE FIRST FLOOR EMERGENCY LIGHT STRIP IAW EMB 145 MM 33-50-12. OPS CHECK GOOD. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20070520015369I](https://openairdocs.org/incident/20070520015369I), May 20, 2007: Emb EMB145LR (N298SK), Richmond, VA, No damage. (-23) Approximately 2339 EDT the aircraft, while enroute from phl to gso, diverted and landed on runway 2 at ric after reporting a fire warning indication in… --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.